General

General

Aero-Mechanical Simulation of Turbomachinery Blading

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      Complete simulation process to design reliable turbomachinery blades. The first step is a full Computational Fluid Dynamics (CFD) of the blade passage to to determine key performance indicators like total pressure ratio and isentropic efficiency along the entire speedline. The second step is a Multiphysics Aero-Mechanical simulation workflow to ensure that all blade natural frequencies and modes of vibration are aerodynamically damped. The third step is also a Multiphysics simulation workflow to determine the stresses caused by the unsteady flow pressure fluctuations on the blade